EP0179137A1 - Procede de formation d'articles composites de formes complexes. - Google Patents

Procede de formation d'articles composites de formes complexes.

Info

Publication number
EP0179137A1
EP0179137A1 EP85902322A EP85902322A EP0179137A1 EP 0179137 A1 EP0179137 A1 EP 0179137A1 EP 85902322 A EP85902322 A EP 85902322A EP 85902322 A EP85902322 A EP 85902322A EP 0179137 A1 EP0179137 A1 EP 0179137A1
Authority
EP
European Patent Office
Prior art keywords
fibers
matrix
forming
yarn
reinforcing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP85902322A
Other languages
German (de)
English (en)
Other versions
EP0179137A4 (fr
EP0179137B1 (fr
Inventor
George K Layden
Karl M Prewo
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
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Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of EP0179137A1 publication Critical patent/EP0179137A1/fr
Publication of EP0179137A4 publication Critical patent/EP0179137A4/fr
Application granted granted Critical
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Classifications

    • C—CHEMISTRY; METALLURGY
    • C03—GLASS; MINERAL OR SLAG WOOL
    • C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B37/00—Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
    • C03B37/10—Non-chemical treatment
    • C03B37/14—Re-forming fibres or filaments, i.e. changing their shape
    • C03B37/15—Re-forming fibres or filaments, i.e. changing their shape with heat application, e.g. for making optical fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
    • C—CHEMISTRY; METALLURGY
    • C03—GLASS; MINERAL OR SLAG WOOL
    • C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C14/00—Glass compositions containing a non-glass component, e.g. compositions containing fibres, filaments, whiskers, platelets, or the like, dispersed in a glass matrix
    • C03C14/002—Glass compositions containing a non-glass component, e.g. compositions containing fibres, filaments, whiskers, platelets, or the like, dispersed in a glass matrix the non-glass component being in the form of fibres, filaments, yarns, felts or woven material
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B30/00—Compositions for artificial stone, not containing binders
    • C04B30/02—Compositions for artificial stone, not containing binders containing fibrous materials
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/64—Burning or sintering processes
    • C04B35/645—Pressure sintering
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71—Ceramic products containing macroscopic reinforcing agents
    • C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
    • C04B35/80—Fibres, filaments, whiskers, platelets, or the like
    • C—CHEMISTRY; METALLURGY
    • C03—GLASS; MINERAL OR SLAG WOOL
    • C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C2214/00—Nature of the non-vitreous component
    • C03C2214/02—Fibres; Filaments; Yarns; Felts; Woven material
    • C—CHEMISTRY; METALLURGY
    • C03—GLASS; MINERAL OR SLAG WOOL
    • C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C2214/00—Nature of the non-vitreous component
    • C03C2214/20—Glass-ceramics matrix
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52—Constituents or additives characterised by their shapes
    • C04B2235/5208—Fibers
    • C04B2235/5216—Inorganic
    • C04B2235/522—Oxidic
    • C04B2235/5224—Alumina or aluminates
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52—Constituents or additives characterised by their shapes
    • C04B2235/5208—Fibers
    • C04B2235/5216—Inorganic
    • C04B2235/522—Oxidic
    • C04B2235/5228—Silica and alumina, including aluminosilicates, e.g. mullite
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52—Constituents or additives characterised by their shapes
    • C04B2235/5208—Fibers
    • C04B2235/5216—Inorganic
    • C04B2235/524—Non-oxidic, e.g. borides, carbides, silicides or nitrides
    • C04B2235/5244—Silicon carbide
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52—Constituents or additives characterised by their shapes
    • C04B2235/5208—Fibers
    • C04B2235/5216—Inorganic
    • C04B2235/524—Non-oxidic, e.g. borides, carbides, silicides or nitrides
    • C04B2235/5248—Carbon, e.g. graphite
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52—Constituents or additives characterised by their shapes
    • C04B2235/5208—Fibers
    • C04B2235/5252—Fibers having a specific pre-form
    • C04B2235/5256—Two-dimensional, e.g. woven structures
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52—Constituents or additives characterised by their shapes
    • C04B2235/5208—Fibers
    • C04B2235/5268—Orientation of the fibers
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32—Ceramic
    • C04B2237/34—Oxidic
    • C04B2237/341—Silica or silicates
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32—Ceramic
    • C04B2237/38—Fiber or whisker reinforced

Definitions

  • the field of art to which this invention pertains is molding processes, and particularly molding processes for forming fiber reinforced composite articles.
  • such techniques incorporate the preparation of the matrix material into a slurry with an organic binder, drawing the reinforcing fibers through the slurry, coating the fibers, winding the coated fibers on a take-up reel, and drying the coated fibers forming a matrix impregnated tape.
  • the matrix impregnated tape is then cut into desired lengths or shapes and laid up in proper fiber orientation, after which they are placed in an oven to burn off the binder. Then the lay-up is carefully placed in a mold and densified under heat and pressure forming the composite.
  • the present invention discloses a method of making fiber reinforced composite articles comprising forming a glass, glass-ceramic or ceramic matrix material into fibers, forming these fibers into yarn, then weaving, braiding, or knitting the yarn into a homogenous cloth of the matrix material. Preparing fibers of reinforcing material; preparing yarns of the reinforcing fibers and then knitting or weaving these yarns into a homogenous cloth of fiber reinforcement. Cutting a plurality of preforms of predetermined shape from each of the cloths, interleaving the fiber reinforcing cloth preforms with one or more layers of the matrix cloth preforms forming a lay-up; placing this lay-up in a die and densifying it under heat and pressure to form the composite article.
  • Another aspect of this invention is the formation of a hybrid cloth material, which is formed by weaving or knitting the yarns of both the glass, glass-ceramic or ceramic matrix material and the fiber reinforcement material into a single cloth; cutting a plurality of preforms of pre ⁇ determined shape from this cloth, stacking the preforms to form a lay-up, placing the lay-up in a die and densifying it under heat and pressure to form the composite article.
  • Yet another aspect of this invention is the formation of an alternative hybrid cloth to that described above using a hybrid yarn comprising fibers of matrix material and fibers of reinforcement material, knitting or weaving these yarns to form a cloth, cutting a plurality of preforms of predetermined shape form this hybrid cloth, stacking said preforms to form a lay-up, placing the lay-up in a die and densifying it to form the composite article.
  • Still yet another aspect of the present invention is the knitting or braiding of a near net structure of continuous matrix yarn and continuous reinforcing fibers or yarn, then densifying the structure in a die to form the composite article.
  • Figure 1 shows a typical cloth fabric of matrix yarn material.
  • Figure 2 shows a typical cloth fabric of fiber reinforcing yarn.
  • Figures 3 and 4 show a typical cloth fabric comprising yams of both matrix and fiber reinforcing material.
  • Figure 5 shows a typical hybrid cloth wherein the yarns comprise a mixture of matrix fibers and reinforcing fibers.
  • Figure 6 shows a cross section of a hybrid yarn comprising both matrix and reinforcing fibers.
  • any glass, glass-ceramic or ceramic material which can be formed into fibers may be used as the matrix material.
  • the choice of which material to use as a matrix will depend on the particular properties desired in the final composite article. Some of the matrices will have greater thermal stability, or higher fracture toughness or be more compatible with a particular reinforcing fiber. These features as well as others will determine which matrix to select. For instance, when forming a composite of glass-ceramic matrix and silicon carbide fibers, the matrix material must be sub ⁇ stantially titanium free in order to form a satisfactory composite.
  • a number of glass matrices which may prove useful in practicing this invention are E-Glass, Corning 1723 aluminosilicate glass, Corning 7740 borosilicate glass and Corning 7930 high silica content glass (96% by weight silica) .
  • some glass-ceramic matrices are lithium aluminosilicate, aluminosilicate and magnesium aluminosilicate, while a representative ceramic material is mullite.
  • the glass, glass-ceramic or ceramic matrix is then formed into continuous fibers by any conventional technique, such as spinning.
  • the diameters and lengths of the fibers which are produced are not critical, nor is the shape (i.e. flat, oval or circular, etc.). However, it is preferred that the fibers be substantially round in shape and have a diameter ranging from about 1 micron to about 25 microns, with 5 to 15 microns preferred. It is important to form the matrix into a fiber which may then be formed into a yarn which may be woven, braided or knitted into a cloth using conventional techniques.
  • the yarn may comnrise a single monofilament fiber or comprise as many as several hundred or more fibers. Typically, the yarn contains about 250 fibers or more.
  • the fiber reinforcement may be any conventional composite reinforcement materials, i.e. carbon, graphite, silicon carbide, alumina, etc. , and may be formed using any of the conventional fiber forming techniques, i.e. drawing, spinning, etc.
  • the limiting factor in selecting the reinforcement material is its thermal compatibility with the temperatures required to densify the matrix and the physical compatibility, (i.e. coefficients of thermal expansion should be closely matched, reactivity, etc.), between it and the matrix.
  • the particular reinforcement material chosen will also depend on the properties desired in the final composite article. Again the diameter, length and design of the fibers is not critical.
  • the fibers be substantially round and have a diameter ranging from about 5 microns to about 200 microns with about 5 to about 150 microns ⁇ referred.
  • the reinforcing continuous fibers may then be formed into yarn comprising, typically, as many as 250 or more fibers. Such yarn should be formed such that it may then be woven or knitted or braided into a cloth using conventional techniques.
  • monofilament fibers may be used to braid, weave or knit the cloth directly, thereby eliminating the extra step of forming the yarn. It is felt that such fibers would have larger diameters than those used for production of the yarns. In addition, such fibers should have the flexibility and strength to allow them to be used in these braiding, weaving and knitting processes.
  • the yarns of matrix fibers and reinforcement fibers are then woven or knitted to form a cloth.
  • This cloth may be homogenous in nature as shown in Figs. 1 and 2. These cloths contain all matrix yarn 10 or all reinforcement yarn 12 respectively.
  • the weaving may be performed using conventional techniques yielding conventional weave patterns such
  • the cloth will be knitted in warp or weft design. These cloths are prepared such that the fibers are oriented substantially at 90° to each other. However, this invention should not be so limited and it may be desirable to form the cloth such that the fibers are oriented at any of a variety of multiple angles, such as 0/ ⁇ 30°, 0/ ⁇ 60°, 0/ ⁇ 45°, or 0/ ⁇ 45°/90°.
  • the cloth may also be formed as a hybrid cloth (Figs. 3 and 4) having a mixture of matrix yarn 10 and reinforcement yarn 12. In preparing such cloth, it does not matter which yarn is used for # the warp and which is used for the weft.
  • the matrix material present in the cloth typically ranges from about 30% to about 70% by volume of solids, with a preferred range of about 40% to about 607 o by volume of solids. Therefore, these cloths will result in a composite article having the desired matrix material content which is typically from about 307 o to about 70% with 40% to 60% by volume preferred.
  • preforms are cut from each of the cloths and stacked to form a lay-up. Since composite articles typically comprise from about 30% to about 70% by volume of matrix material with a preferred range of about 407 o to about 60% by volume, the number of preforms placed in the lay-up should be chosen in order to form a composite having this makeup.
  • lay-up is then placed in a conventional, densifying die and densified under sufficient pressure and temperature to cause the matrix material to flow substantially uniformly around the fiber reinforcement. It should be noted that the interleaving step during the formation of the lay-up is not necessary where a hybrid cloth of the matrix material and reinforcement material is used, because the matrix is already intimately distributed throughout the lay-up.
  • the densification process for the hybrid cloth lay-ups and the homogenous cloth lay-ups is the same.
  • the temperatures, pressures and residence times to which the lay-ups are subjected should be high enough to soften the matrix material and cause it to flow around the fibers but not so high so as to damage the reinforcing fibers themselves.
  • the pressure ranges from about 1.7 to about 13.8 MPa (250 to 2,000 psi) and temperatures of about 1050°C to about 1700°C with residence times of about 15 minutes for glass, glass-ceramic matrices, or ceramic matrices.
  • a preferred pressure range is about 3.4 MPa to about 6.9 while a preferred temperature range is from about 1100°C to 1500°C.
  • Also encompassed in the scope of this invention is the process of forming, by weaving, knitting or braiding, a near net structure co ⁇ prised of con ⁇ tinuous fibers or yarn of both the reinforcing and matrix materials.
  • the yarns or fibers used may be any of the combinations described herein.
  • This weaving, knitting or braiding results in an article with continuous fibers throughout the resulting composite structure.
  • Such three-dimensional articles may be initially formed using conventional knitting techniques with the preferred being the Magnaweave process, described in U.S. Patent 4,312,261 and is incorporated herein by reference.
  • This process achieves the total three-dimensional integration of the yarns or fibers by using an orthogonal shedding motion which is followed by a combing or compacting motion. This process allows for a high degree of freedom in the control of yarn or fiber distribution or orientation, to form the near net structure.
  • the structure is then placed in an appropriate die and densified under suf- ficent temperature and pressure to cause the matrix to flow about the fibers forming the composite article.
  • the total weight of the glass was 24.56 g.
  • the squares were laid up one on top of the other in the sequence of one square of Thornel, then two squares of glass, then one square of
  • the lay-up was complete, it was then ⁇ placed in a conventional graphite hot press die assembly which had been lightly coated with boron nitride which acts as a release agent. A piece of molybdenum foil was placed between the die plunger and the lay-up also to facilitate releasing the composite from the mold.
  • the die assembly was then placed in a hot press and heated to a temperature of about 1350°C. When the temperature of the plunger reached 1100°C, the pressure was raised to 1000 psi. The composition was kept under pressure at elevated temperature for fifteen minutes, then while still under pressure, the heater was turned off and the die was cooled to about 400°C. The pressure was then removed and after the composite had cooled to room temperature (about 25°C) , it was removed from the die.
  • a cross-section of the composite showed excellent penetration and distribution of the glass matrix throughout the composite.
  • the physical properties (i.e. flexural strength 9,000-15,000 psi) of the composite formed using this method were the same as those expected when the composite is prepared using more conventional methods and these materials.
  • the present method offers an alternate technique to forming fiber reinforced articles having a glass, glass-ceramic or ceramic matrix. This method will allow for the elimination of a number of labor intensive and costly steps in the preparation of such articles. This is done by eliminating the preparation of a slurry of the matrix and then coating the fibers to form a tape which may then be formed into the shape of the articles and densified. In addition, an organic binder is typically used in the preparation of these tapes and must be removed prior to densification.
  • the present method offers greater uniformity and control over the matrix material during the lay-up and in the final composite article.
  • this method offers an easier way to make complex, three-dimensional composite articles.
  • the improved purity of the resultant composite, by removal of the need for a fugitive binder, is also of great importance.
  • the process employing the braided or knitted near net structures allows for the formation of complex configured composite articles with superior properties due to the interweaving of the continuous yarns or fibers within the composite article. Such a process lends itself to computer aided design of such structures as I-beams, channels, tubes, etc.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Structural Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Inorganic Chemistry (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Woven Fabrics (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

Procédé de formation d'articles composites matriciels en céramique, verre-céramique ou verre renforcés par des fibres. Le procédé consiste à transformer le matériau matriciel en fibres puis en un fil (10) qui est tissé ou tricoté en une toile. La toile matricielle est ensuite découpée en formes préétablies lesquelles sont entrelacées avec des pièces préformées de tissus qui ont été tissées ou tricotées à partir du fil (12) contenant le renforcement de fibre. Le fil (10, 12) constitué de la fibre de renforcement (12) et des fibres matricielles (10) peut être transformé en une toile hybride. Il est possible de former une toile hybride comprenant le fil (14) des fibres matricielles (16) et de renforcement (18), ou une structure de filet serrée de ces fibres (16, 18) et fils (10, 12). La structure préformée est ensuite placée dans une matrice et densifiée dans des conditions de pression et de température pour former l'article composite.
EP85902322A 1984-04-20 1985-04-19 Procede de formation d'articles composites de formes complexes Expired - Lifetime EP0179137B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/602,284 US4613473A (en) 1984-04-20 1984-04-20 Method for forming composite articles of complex shapes
US602284 1984-04-20

Publications (3)

Publication Number Publication Date
EP0179137A1 true EP0179137A1 (fr) 1986-04-30
EP0179137A4 EP0179137A4 (fr) 1986-07-29
EP0179137B1 EP0179137B1 (fr) 1990-01-17

Family

ID=24410738

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85902322A Expired - Lifetime EP0179137B1 (fr) 1984-04-20 1985-04-19 Procede de formation d'articles composites de formes complexes

Country Status (5)

Country Link
US (1) US4613473A (fr)
EP (1) EP0179137B1 (fr)
JP (1) JPS61501910A (fr)
DE (1) DE3575392D1 (fr)
WO (1) WO1985004835A1 (fr)

Families Citing this family (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4734146A (en) * 1986-03-31 1988-03-29 Rockwell International Corporation Method of producing a composite sine wave beam
US4741873A (en) * 1986-04-15 1988-05-03 Kaiser Aerotech, A Division Of Sowa & Sons Method for forming rigid composite preforms
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EP0179137A4 (fr) 1986-07-29
EP0179137B1 (fr) 1990-01-17
DE3575392D1 (de) 1990-02-22
JPS61501910A (ja) 1986-09-04
US4613473A (en) 1986-09-23
JPH0244270B2 (fr) 1990-10-03
WO1985004835A1 (fr) 1985-11-07

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